We present algorithms for attitude guidance and economical digital control of an information satellite at initial modes – during from its separation from a launcher rocket up to its regular attitude stabilization in orbital reference frame. We represent the computer simulation results on the initial orientation modes of a land-survey satellite on sun-synchronous orbit.
Spacecraft attitude guidance and economical digital control in initial modes
ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia
AIP Conference Proceedings ; 2046 , 1
2018-12-04
7 pages
Conference paper
Electronic Resource
English
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